DocumentCode
3112367
Title
Robust Stability in a Classical and Modern Context
Author
Halsey, Kelvin M.
Author_Institution
Department of Electrical and Electronic Engineering, University of Melbourne, Melbourne, VIC 3010, Australia (e-mail: kmhalsey@ieee.org).
fYear
2005
fDate
12-15 Dec. 2005
Firstpage
2308
Lastpage
2313
Abstract
Excluding the open loop gain of a feedback system from a region about the origin of the Nichols chart yields a natural guarantee of robust stability which is commonly used in the analysis of flight control systems. This paper shows that a generalised form of M-circle, based upon a contour of constant |S| + |T|, is symmetrical on the Nichols chart and yields a stability margin consistent with the gain and phase margin requirements of the USAF. This new margin, motivated on purely classical grounds, is shown to be equal to the robust stability margin associated with the loopshaping design procedure of McFarlane and Glover. A corresponding interpretation is obtained for the multivariable case.
Keywords
Aerospace control; Australia; Control system analysis; Feedback loop; Frequency; Kelvin; Low-frequency noise; Robust stability; Stability criteria; Transfer functions;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2005 and 2005 European Control Conference. CDC-ECC '05. 44th IEEE Conference on
Print_ISBN
0-7803-9567-0
Type
conf
DOI
10.1109/CDC.2005.1582506
Filename
1582506
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